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Please use this identifier to cite or link to this item: http://hdl.handle.net/11375/18085
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DC FieldValueLanguage
dc.contributor.advisorEmadi, Ali-
dc.contributor.authorHeinrich, Maximilian Theobald Ewald-
dc.date.accessioned2015-09-24T15:13:55Z-
dc.date.available2015-09-24T15:13:55Z-
dc.date.issued2015-11-
dc.identifier.urihttp://hdl.handle.net/11375/18085-
dc.description.abstractThis research introduces a high-performance electric taxiing system (ETS) as a modern solution to improve the on-ground operations of today’s aircraft, which are conventionally powered through the main engines. The presented ETS is propelled by electric motors, integrated into the main landing gear of a state-of-the-art midsize commercial aircraft, and powered by an additional not quantified electrical energy storage system. The proposed system can therefore operate autonomously from any aircraft-internal power source, i.e. Auxiliary Power Unit or equivalent. The main objective of this work is to assess the energy consumption of the introduced ETS while considering energy recuperation due to regenerative braking. The ETS powertrain is sized to match modern conventional taxi performances that were seen in 36 self-recorded takeoff- and landing taxi driving profiles. A custom ETS simulation model was developed and simulated across all available driving profiles to confirm the desired powertrain performance and to predict the system’s energy consumption. For the purpose of enhancing the validity of these energy consumption predictions, a suitable motor controller is then designed by the use of MATLAB Simulink. An easy-to-implement switch loss model was created to predict the ETS motor controller efficiency map. Finally, the former energy consumption predictions were revised for the implementation of the motor controller and an estimated traction motor efficiency map. The results exhibit that the revised ETS simulation model was capable of refining the energy consumption. It was found that the ETS will consume up to 9.89 kWh on average if the full potential of the traction motors energy recuperation capabilities are being used. The simulation outcomes further demonstrate that regenerative braking offers great potential in ETS applications since more than 14 % of required traction energy could be regenerated to yield the above mentioned average energy consumption.en_US
dc.language.isoen_USen_US
dc.subjectElectric Taxiingen_US
dc.subjectGreen Taxiingen_US
dc.subjectGreen Taxien_US
dc.subjectPowertrain Designen_US
dc.subjectElectric Taxiing System (ETS)en_US
dc.subjectSystem Sizingen_US
dc.subjectMore Electric Aircraften_US
dc.subjectSimulationen_US
dc.subjectModel-Based Designen_US
dc.subjectAircraft Taxiing Drive Cyclesen_US
dc.subjectKinematic Analysisen_US
dc.subjectRequirements Analysisen_US
dc.subjectRegenerative Brakingen_US
dc.subjectPower Electronicsen_US
dc.subjectMotor Controlsen_US
dc.subjectInverteren_US
dc.subjectSwitch Loss Modelen_US
dc.subjectEfficiency Mapen_US
dc.titleOn the Concept of Electric Taxiing for Midsize Commercial Aircraft: A Power System and Architecture Investigationen_US
dc.typeThesisen_US
dc.contributor.departmentMechanical Engineeringen_US
dc.description.degreetypeThesisen_US
dc.description.degreeMaster of Applied Science (MASc)en_US
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